An experimental investigation of hypersonic turbulent boundary layers in adverse pressure gradient.
- 1 January 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (1) , 105-116
- https://doi.org/10.2514/3.5042
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
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